View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 07665U 75012B 22183.90701887 .00000000 00000-0 20944-3 0 9997
2 07665 69.2301 13.1374 0023619 325.3398 136.1919 12.70416930197437
| Epoch (UTC): | 02 July 2022 21:46:06 |
| Eccentricity: | 0.0023619 |
| inclination: | 69.2301° |
| perigee height: | 1362 km |
| apogee height: | 1398 km |
| right ascension of ascending node: | 13.1374° |
| argument of perigee: | 325.3398° |
| revolutions per day: | 12.70416930 |
| mean anomaly at epoch: | 136.1919° |
| orbit number at epoch: | 19743 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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